Grant: Discovery Grants Program - Individual
Concordia University
$45,000.00
Stress analysis and vibration of elastic and viscoelastic systems (Composite materials and structures)
FY 2015-16
Summary
The first objective of this research program is to provide an integrated design and manufacturing procedure for the development of advanced composite structures that offer high performance, cost efficiency, low wastage, and sensing capability that can detect and locate the occurrence of damages in-situ. The second objective is the development of composite structures that have variation in fiber orientation within a layer (in addition to changes in fiber orientation across layers).
The work for the first objective will involve the incorporation of nanoparticles into the matrix resin of the polymer composites to enhance the fracture toughness, electrical conductivity, and thermal conductivity of the polymer matrix. This modified polymer matrix is then incorporated into long fibers such as carbon fibers, and glass fibers using a prepreg machine. The combined modified matrix and fibers will be processed using automated fiber placement machine to make composite structures of common shapes such as plates, shells or tubes. The use of machines for processing improves the uniformity of the material properties throughout the structure. The enhanced electrical conductivity of the materials will be utilized to provide sensing capability. This sensing capability will enable the detection and location of incurring damages while the structure is in operation (i.e. in-situ or in-flight damage detection and location). The advantage of this method as compared to current NDT technologies is that the material is sensitive at every point in the structure, which makes the sensing to be universal, rather than local.
The work for the second objective will involve the steering of fibers within a layer. This allows the ability to vary the fiber orientation not only across the layers but also within a layer. Optimizaton procedure will be developed to augment the capability of composite structures using this new approach. The use of automated fiber placement machine allows the manufacturing of such a structure. Testing will be done to validate the theories. Step advances for composite materials and structures developments will be made.
Program
Discovery Grants Program - Individual
Recipient
Location
Quebec, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
413-2012
Name nom
Hoa, SuongVan
Department département
Mechanical and Industrial Engineering
Organization id
70
Institution établissement
Concordia University
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2015
Competition year année de concours
2012
Award amount
45000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
Discovery grants programs
Group fr
Programmes de subventions à la découverte
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2100
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Mechanical engineering
Research subject fr
Génie mécanique
Partie
4
Nb partie
5
Application title
Stress analysis and vibration of elastic and viscoelastic systems (Composite materials and structures)
Keyword
NSERC
Application summary
The first objective of this research program is to provide an integrated design and manufacturing procedure for the development of advanced composite structures that offer high performance, cost efficiency, low wastage, and sensing capability that can detect and locate the occurrence of damages in-situ. The second objective is the development of composite structures that have variation in fiber orientation within a layer (in addition to changes in fiber orientation across layers).
The work for the first objective will involve the incorporation of nanoparticles into the matrix resin of the polymer composites to enhance the fracture toughness, electrical conductivity, and thermal conductivity of the polymer matrix. This modified polymer matrix is then incorporated into long fibers such as carbon fibers, and glass fibers using a prepreg machine. The combined modified matrix and fibers will be processed using automated fiber placement machine to make composite structures of common shapes such as plates, shells or tubes. The use of machines for processing improves the uniformity of the material properties throughout the structure. The enhanced electrical conductivity of the materials will be utilized to provide sensing capability. This sensing capability will enable the detection and location of incurring damages while the structure is in operation (i.e. in-situ or in-flight damage detection and location). The advantage of this method as compared to current NDT technologies is that the material is sensitive at every point in the structure, which makes the sensing to be universal, rather than local.
The work for the second objective will involve the steering of fibers within a layer. This allows the ability to vary the fiber orientation not only across the layers but also within a layer. Optimizaton procedure will be developed to augment the capability of composite structures using this new approach. The use of automated fiber placement machine allows the manufacturing of such a structure. Testing will be done to validate the theories. Step advances for composite materials and structures developments will be made.